1995
DOI: 10.1016/0960-0779(94)00172-m
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Mechanical and numerical modelling of fluid-structure vibration instabilities of liquid propelled launch vehicle

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Cited by 27 publications
(2 citation statements)
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“…The two boundary value problems expressed in terms of p or in terms of 𝜑 are well posed in the static case (𝜔 = 0). They have been used, with further transformation, leading to appropriate so-called (u, p,𝜑) symmetric formulations with mass coupling (leading to a final (u,𝜑) formulation, as described by Ohayon and Morand (1995), Chapter 8 or with stiffness coupling, by Sandberg and Goransson (1988).…”
Section: Equationsintermsofp or 𝝋 And U ⋅ Nmentioning
confidence: 99%
“…The two boundary value problems expressed in terms of p or in terms of 𝜑 are well posed in the static case (𝜔 = 0). They have been used, with further transformation, leading to appropriate so-called (u, p,𝜑) symmetric formulations with mass coupling (leading to a final (u,𝜑) formulation, as described by Ohayon and Morand (1995), Chapter 8 or with stiffness coupling, by Sandberg and Goransson (1988).…”
Section: Equationsintermsofp or 𝝋 And U ⋅ Nmentioning
confidence: 99%
“…First, the presence of a free surface in partially filled fluid tanks engenders relative fluid motions to the tank. This phenomenon, referred to as 'fluid sloshing' [5,6], is generally caused by external tank excitation, and may have a significant influence on the response of the tank. Currently, for enhancing the transport ability of space, the ratio of propellant weight to gross liftoff weight almost is up to 90%, thus a rather large perturbation force, moment and impact action introduced by the sloshing of a mass of propellant will exceed the regulating capacity of control system or the bearing capacity of structures.…”
Section: Introductionmentioning
confidence: 99%